A. 50 m
B. 100 m
C. 150 m
D. 250 m
Related Mcqs:
- Assertion A: The width of a taxiway is smaller than the runway width. Reason R : The speed of the aircraft on a taxiway is greater than that on runway.?
Select your answer based on coding system given below
A. Both A and R are true and R is the correct explanation of A
B. Both A and R are true but R is not the correct explanation of A
C. A is true but R is false
D. A is false but R is true - As per International Civil Aviation Organization (ICAO) recommendation, minimum width of safety area for instrumental runway should be_________________?
A. 78 m
B. 150 m
C. 300 m
D. 450 m - The width and interval of transverse centre line bars along the extended centre line of runway, in approach lighting system are_________________?
A. 3 m and 30 m
B. 4.2 m and 30 m
C. 4.2 m and 50 m
D. 3 m and 45 m - For supersonic transport aircraft, the minimum turning radius of taxiway is________________?
A. 60 m
B. 120 m
C. 180 m
D. 240 m - As per ICAO, the minimum basic runway length for A and E type of airport will be________________?
A. 1500 m and 600 m
B. 2100 m and 750 m
C. 1500 m and 750 m
D. 2100 m and 600 m - The total length of a runway is 1000 m. The elevation at distance 0,200 m, 400 m, 600 m, 800 m and 1000 m are 100.0 m, 99.2 m, 101.0 m, 101.8 m, 101.4 m and 101.0 m respectively. The effective gradient of runway will be______________?
A. 0.10%
B. 0.26%
C. 0.43 %
D. 0.65% - For determining the basic runway.length, the landing case requires that aircraft should come to a stop within p % of the landing distance. The value of p is________________?
A. 40 %
B. 50%
C. 60%
D. 75% - The slope of the transitional surface for A, B and C type of runway shall be_______________?
A. 1:5
B. 1:7
C. 1:10
D. 1:12 - Castor angle is defined as the angle______________?
A. formed by the longitudinal axis of the aircraft and the direction of movement of the nose gear
B. between the direction of wind and the longitudinal axis of the runway
C. between the true speed of the aircraft and the crosswind component
D. between the horizontal and the fuselage axis - Assertion A : Airport capacity during IFR conditions is usually less than that during VFR conditions. Reason R: During clear weather condition (VFR), the aircrafts on final approach to runway can be spaced closer during poor visibility conditions?
Select your answer based on the coding system given below?
A. Both A and R are true and R is the correct explanation of A
B. Both A and R are true but R is not the correct explanation of A
C. A is true but R is false
D. A is false but R is true
